Dynamic effects on the transition between two-dimensional regular and Mach reflection of shock waves in an ideal, steady supersonic free stream
From MaRDI portal
Publication:2891627
DOI10.1017/jfm.2011.58zbMath1241.76317OpenAlexW2150067748MaRDI QIDQ2891627
Publication date: 15 June 2012
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://semanticscholar.org/paper/e6f0671e09d3744b2fac08acb29a4abe78ed02b7
Related Items (5)
Unsteady effects of strong shock-wave/boundary-layer interaction at high Reynolds number ⋮ Transition study for asymmetric reflection between moving incident shock waves ⋮ Dynamics of unsteady asymmetric shock interactions ⋮ Numerical and experimental investigation of oblique shock wave reflection off a water wedge ⋮ The non-stationary hysteresis phenomenon in shock wave reflections
Cites Work
- A sequel to AUSM: AUSM\(^ +\)
- Shock wave reflection phenomena
- On the stability of steady-flow regular and Mach reflection
- Investigation of the hysteresis phenomena in steady shock reflection using kinetic and continuum methods
- Numerical confirmation of the hysteresis phenomenon in the regular to the Mach reflection transition in steady flows
- Numerical investigations of transition between regular and Mach reflections caused by free-stream disturbances
- Experiments on shock wave reflection transition and hysteresis in low-noise wind tunnel
- Engineering approach to the prediction of shock patterns in bounded high-speed flows
- Hysteresis effect in stationary reflection of shock waves
- Three-dimensional effects in wind tunnel studies of shock wave reflection
- Irregular effects on the transition from regular to Mach reflection of shock waves in wind tunnel flows
- Analytical and experimental investigations of the reflection of asymmetric shock waves in steady flows
- Experiments on the mechanism of inducing transition between regular and Mach reflection
- Transition between regular and Mach reflection of shock waves: New numerical and experimental results
This page was built for publication: Dynamic effects on the transition between two-dimensional regular and Mach reflection of shock waves in an ideal, steady supersonic free stream
